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Fatigue deformation of a superplastic aluminum-zinc eutectoid alloy.

机译:超塑性铝锌共析合金的疲劳变形。

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摘要

The fatigue deformation of a superplastic aluminum-zinc eutectoid alloy was investigated at temperatures of 100 and 200;Two techniques were used for studying the surfaces of fatigue tested specimens: transmission electron microscopy of two-stage carbon replicas and scanning electron microscopy. Selected areas on a surface were examined before fatigue deformation and re-examined after fatigue deformation. To investigate the internal microstructure of fatigue tested specimens thin foils of fatigue tested specimens were examined in the transmission electron microscope.;During fatigue deformation the average peak stress increased with increasing strain rate and grain size. It increased with decreasing temperature. It was almost independent of the plastic strain amplitude.;Interfacial sliding, interphase boundary migration, and intergranular cracking were detected on the surfaces of fatigue tested specimens. Interfacial sliding, which was almost reversible, occurred on (Al)/(Al) and (Zn)/(Zn) grain boundaries and on (Al)/(Zn) interphase boundaries. It did not occur at every grain boundary and interphase boundary, which suggested that grains slid in groups. Interfacial migration was detected at a few interphase boundaries that intersected the surface. Interphase boundaries usually migrated in the direction of the zinc-rich phase. Cracks followed grain boundaries and interphase boundaries. Along an intergranular crack most interfaces were (Zn)/(Zn) grain boundaries and (Al)/(Zn) interphase boundaries.;Grains deformed to accommodate interfacial sliding. Diffusional creep made a significant contribution to the deformation of grains of the zinc-rich phase. Deformation of the aluminum-rich phase involved the glide and climb of dislocations.;Such processes as Ostwald-ripening, interfacial migration, and precipitation of zinc in the aluminum-rich phase, which involve diffusion, occurred during fatigue deformation. They proceeded more rapidly during fatigue deformation than during annealing.
机译:研究了超塑性铝锌共析合金在100和200的温度下的疲劳变形;采用两种技术研究疲劳测试样品的表面:两阶段碳复制品的透射电子显微镜和扫描电子显微镜。在疲劳变形之前检查表面上的选定区域,并在疲劳变形之后重新检查。为了研究疲劳测试样品的内部微观结构,在透射电子显微镜中检查了疲劳测试样品的薄箔。在疲劳变形期间,平均峰值应力随着应变率和晶粒尺寸的增加而增加。它随着温度降低而增加。它几乎与塑性应变幅度无关。在疲劳测试的试样表面上检测到界面滑动,相间边界迁移和晶间裂纹。 (Al)/(Al)和(Zn)/(Zn)晶界以及(Al)/(Zn)相间界几乎发生了可逆的界面滑动。它不是在每个晶界和相间界都发生,这表明晶粒成群滑动。在与表面相交的几个相间边界处检测到界面迁移。相间边界通常向富锌相的方向迁移。裂纹遵循晶界和相间界。沿晶间裂纹的大多数界面为(Zn)/(Zn)晶界和(Al)/(Zn)相界面。晶粒变形以适应界面滑动。扩散蠕变对富锌相晶粒的变形做出了重要贡献。富铝相的变形涉及位错的滑移和爬升;疲劳变形过程中发生了诸如奥斯特瓦尔德-成熟,界面迁移和富铝相中锌沉淀的过程,这些过程涉及扩散。它们在疲劳变形过程中比在退火过程中进行得更快。

著录项

  • 作者

    Bowden, John Wesley.;

  • 作者单位

    University of Toronto (Canada).;

  • 授予单位 University of Toronto (Canada).;
  • 学科 Engineering Materials science.
  • 学位 Ph.D.
  • 年度 1988
  • 页码 1 p.
  • 总页数 1
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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